Solid rocket stage. 170.00 kN (38,218 lbf) thrust. Mass 1,700 kg (3,748 lb).
Status: Retired 1972.
More... - Chronology...
Gross mass: 1,700 kg (3,700 lb).
Unfuelled mass: 455 kg (1,003 lb).
Height: 4.70 m (15.40 ft).
Diameter: 0.56 m (1.83 ft).
Thrust: 170.00 kN (38,210 lbf).
Burn time: 20 s.
Number: 10 .
Associated Launch Vehicles
Tacite French sounding rocket. Single stage sounding rocket using a single Stromboli SEPR 739-2 stage with 'Plastoline' propellant. Stabilisation was by four fins and a nitrogen cold-gas spin thrusters. More...
Titus French sounding rocket. Sounding rocket derived from the first two stages of the Berenice test vehicle. The two stage vehicle consisted of 4 x SEPR P167 stabilisation rockets around a Stromboli 739 first stage, topped by a stretched Stromboli SEPR 740-3 second stage with four fins. The launches were made from Chaco in collaboration with the Argentinian agency CNIE. More...
Tibere French test vehicle. Tibere was an atmospheric re-entry test vehicle derived from the earlier Berenice. Development was authorized in 1965 to support the Electre re-entry experiment program. The first two stages were Stromboli motors of identical length. The third stage was the P.064 motor developed for the Diamant orbital launcher. More...
Associated Manufacturers and Agencies
ONERA French manufacturer of rocket engines and rockets. Office National d'Etudes et de Recherches Aerospatiales, France. More...
Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...
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